TRAIL - Technical Report Archive and Image Library

Wind-Tunnel Tests of a 1/4-Scale Model of the Naval Aircraft Factory Float-Wing Convoy Interceptor, TED No. NACA 2314

Wind-Tunnel Tests of the 1/25-Scale Powered Model of the Martin JRM-1 Airplane. 4 - Tests with Ground Board and with Modified Wing and Hull - TED No. NACA 232, Part 4, Tests with Ground Board and with Modified Wing and Hull, TED No. NACA 232

Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms August 17, 1946 to August 19, 1946 at Orlando, Florida

Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms July 22, 1946 to July 23, 1946 at Orlando, Florida

Two-Dimensional Wind-Tunnel Investigation of Modified NACA 65(sub 112)-111 Airfoil with 35-Percent-Chord Slotted Flap to Determine Pitching-Moment Characteristics and Effects of Roughness

Two-Dimensional Wind-Tunnel Investigation of Modified NACA 65(112)-111 Airfoil with 35-Percent-Chord Slotted Flap to Determine Optimum Flap Configuration at Reynolds Number of 2.4 Million

Two-Dimensional Wind-Tunnel Investigation of Modified NACA 65(sub 112)-111 Airfoil with 35-Percent-Chord Slotted Flap at Reynolds Numbers up to 25 Million

Landing Characteristics in Waves of Three Dynamic Models of Flying Boats

Pressure-Distribution Measurements on a Straight and on a 35 Degree Swept-Back Tapered Wing

Voltera's Solution of the Wave Equation as Applied to Three-Dimensional Supersonic Airfoil Problems

A Ram-Jet Engine for Fighters

Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degree Sweptback Wing at Reynolds Numbers to 8,000,000

Method of Characteristics for Three-Dimensional Axially Symmetrical Supersonic Flows

Investigation of the dynamic response of airplane wings to gusts

An Investigation at Low Speed of a Large-Scale Triangular Wing of Aspect Ratio Two 1: Characteristics of a Wing Having a Double-Wedge Airfoil Section With Maximum Thickness at 20-Percent Chord

Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream

A unified theory of plastic buckling of columns and plates

Considerations of the Total Drag of Supersonic Airfoil Sections

Airfoil in Sinusoidal Motion in a Pulsating Stream

The 1350 F stress-rupture properties of two wrought alloys and three cast alloys

Planing of Watercraft

Flight Measurements of Buffeting Tail Loads

An experimental investigation of the design variables for NACA submerged duct entrances

Air-flow surveys in the vicinity of representative NACA 1-series cowlings

Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps

Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps

An Investigation of the Wing and the Wing-Fuselage Combination of a Full-Scale Model of the Republic XP-91 Airplane in the Ames 40-by 80-Foot Wing Tunnel

Preliminary Results of British Nene II Engine Altitude-Chamber Performance Investigation. I - Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle, 1, Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle

Calculations of the Dynamic Stress of Several Airplane Wings in Various Gusts

Performance of J-33-A-21 Turbojet-Engine Compressor I - Over-All Performance Characteristics at Equivalent Impeller Speeds from 6000 to 13,400 RPM

Comparison of Drop and Wind-Tunnel Experiments on Bomb Drag at High Subsonic Speeds

The Influence of the Diameter Ratio on the Characteristics Diagram of the Axial Compressor

Measurements on Compressor-Blade Lattices

Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine, Part 5, Performance and Windmilling Drag Characteristics

Performance of Compressor of XJ-41-V Turbojet Engine VI - Analysis of Compressor Flow Choking, 6, Analysis of Compressor Flow Choking

Ground Tests of a Radial Air-Cooled Engine to Correct a Poor Circumferential Pressure-Recovery Distribution

Simulated Altitude Performance of Combustor of Westinghouse 19XB-1 Jet-Propulsion Engine

Simulated Altitude Performance of Combustors for the Westinghouse 24C Jet Engine I-24C-2 Combustor

Effect of Distribution of Basket-Hole Area on Simulated Altitude Performance of 25 1/2-Inch-Diameter Annular-Type Turbojet Combustor

Performance of Compressor of XJ-41-V Turbojet Engine, 4, Performance Analysis Over Range of Compressor Speeds from 5000 to 10,000 RPM

Performance of J33-A-23 Turbojet-Engine Compressor, Part 1, Over-All Performance Characteristics of Compressor with 17-Blade Impeller

Performance of J33-A-23 Turbojet-Engine Compressor, II, Over-All Performance Characteristics of Compressor with 34-Blade Impeller at Equivalent Impeller Speeds from 6000 to 11.750 RPM

Theoretical Comparison of Several Methods of Thrust Augmentation for Turbojet Engines

Performance of J-33-A-21 and J-33-A-23 Compressors with and without Water Injection

Tank Tests of a Powered Model of a Compression Plane, NACA Model 171A-2

Natural icing of an axial-flow turbojet engine in flight for a single icing condition

Investigation of Effectiveness of Air-Heating a Hollow Steel Propeller for Protection Against Icing 1: Unpartitioned Blades

Investigation of Effectiveness of Air-Heating a Hollow Steel Propeller for Protection Against Icing. 2: 50% Impartitioned Blades

Investigation of Effectiveness of Air-Heating a Hollow Steel Propeller for Protection Against Icing. 3: 25% Partitioned Blades

An investigation of fretting corrosion under several conditions of oxidation

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